Demonstration of Bipropellant Mode for Microsatellite-Friendly Multi-Purpose Propulsion System

Author:

Sahara Hironori,Kobayashi Yuya,Nakamura Kenjiro,Omata Yukano,Abe Keisuke,Someya Subaru,Nishio Kanta,Iizuka Toshiaki

Publisher

Japan Society for Aeronautical and Space Sciences

Reference13 articles.

1. 1) Heidt, H., Puig-Suari, J., Moore, A. S., Nakasuka, S. and Twiggs, R. J.: A New Generation of Picosatellite for Education and Industry Low-Cost Experimentation, 14th AIAA/USU Conference on Small Satellites, SSC00-V-5, 2000.

2. 3) Forshaw, J. L., Aglietti, G. S., Salmon, T., Retat, I., Roe, M., Burgess, C., Chabot, T., Pisseloup, A., Phipps, A., Bernal, C., Chaumette, F., Pollini, A. and Steyn, W. H.: Final Payload Test Results for the RemoveDebris Active Debris Removal Mission, Acta Astronautica, 138 (2017), pp. 326-342.

3. 4) Dyer, J. M. and McClelland, J.: Paradigm Change in Earth Observation-Skybox Imaging and SkySat-1, Proc. 12th Reinventing Space Conf., 2016, pp. 69-89.

4. 5) Klesh, A. and Krajewski, J.: MarCO: CubeSats to Mars in 2016, 29th AIAA/USU Conference on Small Satellites, SSC15-III-3, 2015.

5. 8) Price, T. W. and Evans, D. D.: The Status of Monopropellant Hydrazine Technology, National Aeronautics and Space Administration Technical Report 32-1227, 1968.

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